JASC 5730

Service difficulty reports · 27,269

Reports filed under 5730 · Wing, Plate/Skin, newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5730'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR IPXA11M68725Doubler · crackedINSPECTION TYPE:4C, LT WING L/E COMPT BEADED DOUBLER IS CRACKED AT 5 EA FASTENERS AT XOS 732 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS732 REF EO MD11- 5730-42916-A.Jul 28, 2011 · N285UP · Doug MD11FSDR IPXA11M68724Doubler · crackedINSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 2EA FASTENERS AT APPX XOS754. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT XOS754 REF EO MD11-5730-42916-A.Jul 28, 2011 · N285UP · Doug MD11FSDR IPXA11M68723Doubler · crackedINSPECTION TYPE:4C, LT WING L/E COMPT CEILING BEADED DOUBLER IS CRACKED AT 3EA FASTENERS AT XOS880 APPROX. REPAIRED LT WING L/E COMPT BEADED DOUBLER AT STA XOS880 REF EO MD11-5730-42916-A.Jul 28, 2011 · N285UP · Doug MD11FSDR UIEA2011072800435Skin · corrodedDURING THE "C4 PLUS A6 CHECK, CORROSION DAMAGE WAS DETECTED AT THE UPPER SURFACE OF RT WING LOWER SKIN PANEL BETWEEN WS 1289 - WS 1312. THE CORROSION DAMAGE WAS SPREAD OVER A WIDTH OF 15" WITH A DEPTH OF 3" AS DOCUMENTED IAW NRC 50723. AFTER BLENDING, THE REJul 28, 2011 · N524MC · Boeing 7472D7BSDR VNAA2011080200031Skin · dentedAT ROA, CREW REPORTED BIRD STRIKE ON LEADING EDGE OF RIGHT WING. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT OUTBOARD LEADING EDGE ASSEMBLY AND PICCOLO DUCT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.Jul 27, 2011 · N249PS · Cndair CL6002B19SDR IPXA11M68692Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT INBD OF SLAT TRACK NR11, BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E COMPT BEADED DOUBLER INBD OF SLAT TRACK NR 11 REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68691Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619EB AREA ABOVE SLAT CABLE PULLEY, BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E COMPT BEADED DOUBLER AT ACCESS 619EB ABOVE SLAT CABLE PULLEY REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68688Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619EB CEILING AREA FOUND BEADED DOUBLER CRACKED. REPAIRED RT WING L/E COMPT BEADED DOUBLER AT ACCESS 619EB REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68686Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT INBD OF SLAT TRACK NR 12 BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E BEADED DOUBLER INBD OF SLAT TRACK NR 12 REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68685Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT OTBD OF SLAT TRACK NR 10 BEADED DOUBLER FOUND CRACKED. REPAIRED RT WING L/E BEADED DOUBLER OTBD OF SLAT TRACK NR 10 REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68684Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619CB AREA ABOVE INBD FUEL RECEPTICAL FOUND BEADED DOUBLER CRACKED. REPAIRED RT WING L/E BEADED DOUBLER AT ACCESS 619CB REF EO MD11-573 0-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68683Doubler · crackedINSPECTION TYPE:4C, RT WING L/E INBD OF SLAT TRACK NR16 BEADED DOUBLER FOUND WITH CRACKS. REPAIRED RT WING L/E BEADED DOUBLER OTBD OF SLAT TRACK 16 REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA11M68682Doubler · crackedINSPECTION TYPE:4C, RT WING L/E COMPT THROUGH ACCESS 619CB AREA ABOVE OTBD FUEL RECEPTICAL FOUND BEADED DOUBLER CRACKED. REPAIRED RT L/E BEADED DOUBLER AT ACCESS 619CB REF EO MD11-5730-42916-A.Jul 26, 2011 · N285UP · Doug MD11FSDR IPXA1M68555Skin Panel · wornINSPECTION TYPE:3C, LT WING L/E LOWER EXTERNAL SKIN HAS DEEP FRETTING WEAR STA 300. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT WING SKIN PANEL AT LT L/E EXTERIOR, STA 300 IAW DWG ARB2363, SRM 51-35-01, 57-40-01.Jul 26, 2011 · N294UP · Doug MD11FSDR IPXA11M68451Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E COMPT STA 772 (APPRX XOS881) INNER SKIN BEADED DOUBLER CRACKED AT SEVERAL FASTENERS. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS879-882 IAW SRM 57-40-02 REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.Jul 26, 2011 · N294UP · Doug MD11FSDR IPXA11M68443Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E COMP'T AT STA 592 (XOS695 APPRX) INNER SKIN BEADED DOUBLER CRACKED AT SEVERAL FASTENERS. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS692-698 IAW SRM 57-40-02, REPAIR 9, FIG 203 AND EO MD11-5730-42916-A.Jul 26, 2011 · N294UP · Doug MD11FSDR IPXA11M68442Doubler · crackedINSPECTION TYPE:3C, LT WING FIXED L/E COMPARTMENT AT STA 627 (XOS731 APPROX) INNER SKIN BEADED DOUBLER CRACKED AT SEVERAL FASTENER LOCATIONS. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS728-735 IAW SRM 57-40-02 REPAIR 9, FIG 203 AND EO MD11-Jul 26, 2011 · N294UP · Doug MD11FSDR FDEA201107262957Skin · crackedRT WING L/E TELESCOPIC DUCT CUTOUT OTBD CORNER SKIN AT XOS 470 FOUND CRACKED. REPAIR CARRIED OUT PER SRM 57-40-01 FIG. 202 REV.47 .REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV.112Jul 26, 2011 · N573FE · Doug MD11FSDR CA110726014Skin · buckledDURING INSP, MX FOUND LT & RT WING SKIN BUCKLED BETWEEN ENGINE NACELLE AND FUSELAGE & LIFTED AT ONE POINT AT MAIN SPAR ATTACHMENT (LIFTED & BUCKLED APPROX. .1250" BETWEEN RIVETS). FURTHER INSP FOUND BUCKLING OF THE MAIN WING SPAR WEBS IN THE LT & RT OTBD WHEELJul 25, 2011 · Piper PA31350SDR A6WA201140749Panel · corrodedLT WING PANEL C/O 550AB HAS INDICATION OF CORROSION INBD. WORKED IAW EO E06/012/457 & REO 601R-57-21-030.Jul 25, 2011 · N420AW · Cndair CL6002B19SDR UALA2011072503794Structure · damagedDAMAGE TO LT WING L/E OTBD. REMOVED AND REPLACED BULLNOSE PANEL. NR 1 L/E SLAT IS DAMAGE. REPLACED NR 1 L/E SLAT.Jul 24, 2011 · N229UA · Boeing 777222SDR VNAA2011072700026Skin · corrodedDURING SCHEDULED MAINTENANCE LEFT WING LOWER PLANK ACCESS HOLE (540BB) WAS PITTED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.Jul 24, 2011 · N260JS · Cndair CL6002B19SDR QXEA2011072500593Access Panel · corrodedLT WING ACCESS PANEL 524CT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442, FOUND WITHIN LIMITS. CONFIRMED CRACK FREE AREA REF RD 8/4-53-442. TREATED AND PRIMED PANEL IAW RD 8/4-57-442.Jul 24, 2011 · N423QX · Bombdr DHC8402SDR FDEA201107232917Skin · corrodedCENTER WING LOWER SKIN BS 1368 (REAR SPAR AREA) CORRODED AT 2EA. LOCATIONS, 12" AND 36" OTBD OF LT KEELBEAM. REMOVED CORROSION ON CENTER WING LWR SKIN IAW EA 8-5710-152431.Jul 23, 2011 · N68051 · Doug MD1010FSDR UALA2011072203726Skin · damagedLEFT WING L/E UPPER SKIN HAS 6 INCH LONG GOUGE FROM CONTACTING NR 3 SLAT OUTBOARD END BLADE SEAL SCREW. DAMAGE IS 12' FROM PANEL INBD EDGE, 5.250 FROM AFT EDGE,4.250" FROM NEAREST FASTENER, AND 13" FROM NEAREST REPAIR. REPAIRED IAW SRM 57-41-01 AND SB 757-5Jul 22, 2011 · N540UA · Boeing 757222SDR UVVR2011072200017Skin · corrodedDURING COMPLIANCE OF SB 99-2 INSPECT LT & RT WING TIPS, LT TOP AND BOTTOM AFT WING PLANK CORRODED AROUND NUT PLATE AREAS AT REAR SPAR (RS) 258.371 TO 270.371.Jul 22, 2011 · N4CS · Rkwell NA26565SDR FDEA201107202831Skin · corrodedLT WING OUTER OVERWING REFUEL ADAPTOR REMOVED, FOUND CORROSION AT TOP SKIN SHROUND (FROM 5 TO 11 O'CLOCK POSITION ). ACCOMPLISHED EA 6-5720-149013. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. CLEANED UP IAW AMM 28-11-00.Jul 20, 2011 · N428FE · Airbus A310203SDR IPXA11M68400Skin · chafedINSPECTION TYPE:3C, LT WING UPPER L/E SURFACE DOUBLER CHAFED AT STA XIS247 (AFTER REMOVAL OF DOUBLER FOUND SEVERAL FASTENER HOLES IN INTERNAL BEADED DOUBLER THAT DO MEET SRM REQUIREMENTS). REPAIRED LT WING UPPER L/E IAW STASA EA 011-5710-01-A3305 REV IR AND EJul 20, 2011 · N293UP · Doug MD11FSDR IPXA11M68389Skin · chafedINSPECTION TYPE:3C, LT WING L/E FROM NR6 SLAT TRACK TO PYLON, 2EA REPAIR DOUBLERS ARE CHAFED. (AFTER REMOVAL OF EXISTING DOUBLERS FOUND SEVERAL OVERSIZED FASTENER HOLES) REPAIRED LT WING FIXED L/E EXTERIOR BETWEEN STA XOS406-420 & XOS421 IAW STASA EA 011-573Jul 20, 2011 · N293UP · Doug MD11FSDR IPXA11M68380Skin · gougedINSPECTION TYPE:3C, SCAB PATCH ON RT WING UPPER L/E APPROX XORS 130.4 (XIS247) IS GOUGED AND CHAFED BY CONTACT WITH NR1 SLAT. REPAIRED RT WING UPPER L/E EXTERIOR SKIN BETWEEN XIS 244-250 IAW SRM 57-40-02, REPAIR 8, FIG 201, STASA EA011-5710-01-A3312 REV IR ANJul 20, 2011 · N293UP · Doug MD11FSDR IPXA11M68319Skin · crackedINSPECTION TYPE:3C, LT WING L/E SKIN ANTI-ICE TELESCOPIC DUCT CUT-OUT HAS A CRACK AT OTBD UPPER CORNER. REPAIRED LT WING FIXED L/E EXTERIOR SKIN AT XOS470 ANTI-ICE DUCT CUT- OUT IAW SRM 57-40-01, REPAIR 10, FIG 201.Jul 20, 2011 · N293UP · Doug MD11FSDR FDEA201107202832Skin · chafedLT WING OUTER OVERWING REFUEL ADAPTOR REMOVED. FOUND CORROSION AT TOP SKIN SHROUND (FROM 5 TO 11 O'CLOCK POSITION ). ACCOMPLISHED EA 6-5730-149017. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 20, 2011 · N428FE · Airbus A310203SDR FDEA201107192786Skin · crackedRT WING FIXED L/E TELESCOPIC DUCT DOOR CUTOUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-01, FIG 202. REPAIR 10, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 19, 2011 · N645FE · Doug MD11FSDR FDEA201107192785Skin · crackedLT WING FIXED L/E TELESCOPIC DUCT DOOR CUTOUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-01 FIG 202, REV 46. REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Jul 19, 2011 · N645FE · Doug MD11FSDR SROM2011006Skin · gougedGOUGE IN RT UPPER INSPAR WING SKIN UPPER SURFACE ABOVE AFT SPAR AT WBL 77R REPAIRED IN ACCORDANCE WITH MESSAGE NOS. KFC-ATR-11-0003-01C, DATED JUNE 23, 2011, KFC-ATR-11-0003-05B, DATED JUNE 29, 2011, KFC-ATR-11-0003-06C, DATED JULY 4, 2011 AND BOEING APPROVEDJul 19, 2011 · N736BP · Boeing 737205SDR SROM2011005Skin · gougedGOUGE IN LT UPPER INSPAR WING SKIN UPPER SURFACE ABOVE AFT SPAR AT WBL 77L REPAIRED IN ACCORDANCE WITH MESSAGE NOS. KFC-ATR-11-0002-01C, DATED JUNE 23, 2011, KFC-ATR-11-0002-07B, DATED JUNE 29, 2011, KFC-ATR-11-0002-08C, DATED JULY 4, 2011 AND BOEING APPROVEDJul 19, 2011 · N736BP · Boeing 737205SDR QXEA2011072700599Access Panel · corrodedLT WING ACCESS PANEL 524BT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION ON LT WING ACCESS PANEL 524BT PAD MATING SURFACE IAW RD 8/4-57-442. REMAINING MATERIAL THICKNESS .117" WITH IN LIMITS IAW RD 8/4-57-442. CONFIRMED CRACK FREE REF RD 8/4-57-4420. TJul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072100542Access Panel · corrodedC2 - LT WING ACCESS PANEL 525AT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. BLENDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-442. COMPLETED REPAIR IAW RD 8/4-57-442.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072100541Access Panel · corrodedC2 - LT WING ACCESS PANEL 524FT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. BLENDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-442. COMPLETED REPAIR IAW RD 8/4-57-442.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072100540Access Panel · corrodedC2 - LT WING ACCESS PANEL 524ET HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. BLENDING FOUND TO BE WITHIN LIMITS IAW RD 8/4-57-442. COMPLETED REPAIR IAW RD 8/4-57-442.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000536Access Panel · corrodedCOE - C2 - LT WING ACCESS LANDING FOR PANEL 525AT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000535Access Panel · corrodedC2 - LT WING ACCESS LANDING FOR PANEL 524FT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000534Access Panel · corrodedC2 - LT WING ACCESS LANDING FOR PANEL 524ET HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000533Access Panel · corrodedC2 - LT WING ACCESS LANDING FOR PANEL 524CT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000532Access Panel · corrodedC2 - LEFT WING ACCESS PANEL 524BT HAS CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000530Access Panel · corrodedC2 - LT WING ACCESS LANDING FOR PANEL 524AT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR REF RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA2011072000529Access Panel · corrodedC2 - LT WING ACCESS LANDING FOR PANEL 524DT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR QXEA20110720528Access Panel · corrodedC2 - LT WING ACCESS LANDING FOR PANEL 524BT HAS CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-445. FOUND REMAINING THICKNESS TO BE WITHIN LIMITS AND COMPLETED REPAIR IAW RD 8/4-57-445.Jul 18, 2011 · N423QX · Bombdr DHC8402SDR FDEA201107172769Skin · misrepairedREPAIR AT LT WING INBD FLAP LOWER SKIN INBD SIDE XIFH 201 TO XIFH 207 EVALUATED AND FOUND PREVIOUSLY NOT ACCOMPLISHED IAW APPROVED DATA. REPAIR REMOVED IAW SRM 51-35-01, REV 47. NEW REPAIR DOUBLER FABRICATED AND INSTALLED IAW SRM 57-00-01, FIG 201, REPAIR 1,Jul 17, 2011 · N642FE · Doug MD11FSDR FDEA201107172772Skin · chafedLT WING ABOVE NR 1 PYLON OTBD SIDE FIXED L/E FOUND WITH CHAFING MARK. FOUND EXCEEDED LIMIT ORIGINAL THICKNESS = 0.090", MATERIAL REMOVED = 0.033", REMAINED THICKNESS = 0.057, DIAMETER = 0.8" X 8" IAW SRM 57-00-00, FIG 202, REV 47. DAMAGED SKIN REMOVED AND NEJul 17, 2011 · N642FE · Doug MD11F
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